Pointing Error Analysis of Star Sensor on GEO Satellite

被引:1
作者
Wu Hankun [1 ]
Xia Yongquan [1 ]
Wu Ruilan [1 ]
机构
[1] China Acad Space Technol, Inst Telecommun Satellite, Beijing, Peoples R China
来源
2018 EIGHTH INTERNATIONAL CONFERENCE ON INSTRUMENTATION AND MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC 2018) | 2018年
关键词
GEO satellite; star senor; pointing error;
D O I
10.1109/IMCCC.2018.00336
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
For geostationary communication satellites, the measurement precision of high accuracy star sensor is an important factor which affects the pointing accuracy of the satellite. Using on-orbit data from the star sensors on different positions of the satellite, we find that the variation of star sensor pointing error is related to the variation of the orbit thermal environment. We compare the thermal deformation simulation result of the installation structure of the star sensor and the on-orbit data. These two agree with each other on the direction and the magnitude of error variation. The conclusion is that the periodical thermal deformation of the star sensor installation structure is the main factor affecting its accuracy.
引用
收藏
页码:1632 / 1636
页数:5
相关论文
共 4 条
[1]   The PROBA satellite star tracker performance [J].
Jorgensen, JL ;
Denver, T ;
Betto, M ;
Van den Braembussche, P .
ACTA ASTRONAUTICA, 2005, 56 (1-2) :153-159
[2]  
Ren Youliang, 2017, Spacecraft Engineering, V26, P77, DOI 10.3969/j.issn.1673-8748.2017.02.011
[3]  
Wang L, 2006, INT J COMPUT SCI NET, V6, P50
[4]   Calibration of transition matrix on cubic prisms in mapping camera and star sensor [J].
Wang, Zhi ;
Wu, Guo-Dong .
Guangxue Jingmi Gongcheng/Optics and Precision Engineering, 2012, 20 (01) :96-101